SPHERES MOSR Rendezvous and Docking with the OS (RDOS)
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AbstractNASA's Mars Sample Return (MSR) mission involves many challenging operations. One of the highest-risk operations is the guidance of the Orbiting Sample (OS) into the capture mechanism on the MSR Orbiter/Earth Return Vehicle (ERV). Aurora Flight Sciences, and its research partner the Massachusetts Institute of Technology (MIT) Space Systems Laboratory (SSL), propose to adapt and augment the Synchronized Position Hold Engage Reorient Experimental Satellites (SPHERES) Mars Orbiting Sample Retrieval MOSR testbed to incorporate optically-guided rendezvous and docking with the OS (RDOS). This additional functionality will extend the MOSR testbed's existing capabilities to further support MSR rendezvous and capture algorithm development. With these new capabilities, the MOSR RDOS system would extend the utility of the MOSR testbed from the "last meter" problem
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